• Acta Photonica Sinica
  • Vol. 53, Issue 11, 1122001 (2024)
Shuai YE1, Yi ZENG1,*, Xiaofeng LU2, Fenglei LIU2..., Lei ZHU2, Jun CHEN2, Yu JIANG2, Minjie ZHAO2, Haijin ZHOU2 and Fuqi SI2|Show fewer author(s)
Author Affiliations
  • 1University of Science and Technology of China,Hefei 230026,China
  • 2Key Laboratory of Environmental Optics and Technology,Anhui Institute of Optics and Fine Mechanics HFIPS,Chinese Academy of Sciences,Hefei 230031,China
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    DOI: 10.3788/gzxb20245311.1122001 Cite this Article
    Shuai YE, Yi ZENG, Xiaofeng LU, Fenglei LIU, Lei ZHU, Jun CHEN, Yu JIANG, Minjie ZHAO, Haijin ZHOU, Fuqi SI. Optimization Design of the Spaceborne Edge Spectral Imager Reflective Mirror Assembly[J]. Acta Photonica Sinica, 2024, 53(11): 1122001 Copy Citation Text show less
    Optical system design
    Fig. 1. Optical system design
    Schematic diagram of the installation location
    Fig. 2. Schematic diagram of the installation location
    Concave mirror assembly structure
    Fig. 3. Concave mirror assembly structure
    Topology optimized regions
    Fig. 4. Topology optimized regions
    Iterative convergence curves
    Fig. 5. Iterative convergence curves
    Topology optimization results
    Fig. 6. Topology optimization results
    Post-process model
    Fig. 7. Post-process model
    Schematic diagram of reinforcement thickness grouping
    Fig. 8. Schematic diagram of reinforcement thickness grouping
    The contribution of the reinforcement thickness of each group to the PV
    Fig. 9. The contribution of the reinforcement thickness of each group to the PV
    Schematic diagram of the structure
    Fig. 10. Schematic diagram of the structure
    Initial design drawings of flexible structure
    Fig. 11. Initial design drawings of flexible structure
    Influence of different structural parameters on Q
    Fig. 12. Influence of different structural parameters on Q
    Results of the gravity load analysis
    Fig. 13. Results of the gravity load analysis
    Results of thermo-mechanical coupling analysis
    Fig. 14. Results of thermo-mechanical coupling analysis
    Three-way vibration pattern
    Fig. 15. Three-way vibration pattern
    On-site test diagram
    Fig. 16. On-site test diagram
    Three-dimensional frequency scanning results
    Fig. 17. Three-dimensional frequency scanning results
    The component surface shape result plot before optimization
    Fig. 18. The component surface shape result plot before optimization
    The component surface shape result plot after optimization
    Fig. 19. The component surface shape result plot after optimization
    Surface shape test results
    Fig. 20. Surface shape test results
    Optimized the point plot after processing
    Fig. 21. Optimized the point plot after processing
    Technical parametersTechnical indicators
    Spectral range500~800 nm
    S/N600@2.8 μW/cm2sr-1 nm-1
    Spectral resolution≤2 nm
    Spatial resolution≤2 km
    Table 1. Optical system indicators
    MaterialDensity ρ/(gcm3Elastic modulus E/GPaPoisson's ratio μ

    Thermal expansion coefficient

    α/(×10-6 K-1)

    Zerodur2.5290.60.240.1
    4J328.051410.360.3
    2A122.7680.3322.5
    Table 2. Material performance indicators
    GroupingRange/mmInitialResultsRounder
    12633.3653.5
    826322
    102633.8194
    132633.8114
    152634.1524.5
    1626322
    172634.1534.5
    182633.9804
    202633.9744
    Table 3. Reinforcement thickness optimization results
    GroupingValue/mm
    13.5
    82
    104
    134
    154.5
    162
    174.5
    184
    204
    2,3,4,5,6,7,9,11,12,14,193
    215
    Mirror thickness21.24
    Table 4. Reflector structure parameter results
    OrderFrequency/HzMode shapes
    1942.2Mirror moves in the Z direction
    21 078.1Mirror rotates around the X direction
    31 118.9Mirror rotates around the Y direction
    41 331.3Mirror rotates around the Z direction
    52 175.9Mirror moves in the Y direction
    62 223.1Mirror moves in the X direction
    Table 5. The results of the first 6-order modal analysis of the mirror assembly
    The frequency rangeOrder of magnitudeScanning rateLoading direction
    5~2 000 Hz0.5 g4 oct/minX,Y,Z
    Table 6. Sine sweep input conditions
    Load caseB.O.PV/nmA.O.PV/nmOptimization rateB.O. RMS/nmA.O. RMS/nmOptimization rate
    Z-1 g50.846.78.0%10.299.57.8%
    Z-1 g+2 ℃47.840.615%10.168.2518.2%
    Table 7. Comparison of surface shape data before and after optimization
    Shuai YE, Yi ZENG, Xiaofeng LU, Fenglei LIU, Lei ZHU, Jun CHEN, Yu JIANG, Minjie ZHAO, Haijin ZHOU, Fuqi SI. Optimization Design of the Spaceborne Edge Spectral Imager Reflective Mirror Assembly[J]. Acta Photonica Sinica, 2024, 53(11): 1122001
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